View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 33499U 09002H 24280.83378400 .00007729 00000-0 10347-2 0 9990
2 33499 98.1259 183.7279 0009719 123.6628 236.5511 14.79695811845051
| Epoch (UTC): | 06 October 2024 20:00:38 |
| Eccentricity: | 0.0009719 |
| inclination: | 98.1259° |
| perigee height: | 623 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 183.7279° |
| argument of perigee: | 123.6628° |
| revolutions per day: | 14.79695811 |
| mean anomaly at epoch: | 236.5511° |
| orbit number at epoch: | 84505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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